US12071998B2 - Cryocooler assemblies and methods - Google Patents
Cryocooler assemblies and methods Download PDFInfo
- Publication number
- US12071998B2 US12071998B2 US16/597,655 US201916597655A US12071998B2 US 12071998 B2 US12071998 B2 US 12071998B2 US 201916597655 A US201916597655 A US 201916597655A US 12071998 B2 US12071998 B2 US 12071998B2
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- Prior art keywords
- assembly
- coldhead
- mass
- cryocooler
- housing
- Prior art date
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- 238000000429 assembly Methods 0.000 title claims abstract description 33
- 230000000712 assembly Effects 0.000 title claims abstract description 33
- 238000000034 method Methods 0.000 title abstract description 10
- 230000033001 locomotion Effects 0.000 claims abstract description 6
- 238000001816 cooling Methods 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 239000007788 liquid Substances 0.000 description 4
- 238000004891 communication Methods 0.000 description 3
- 239000012530 fluid Substances 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
- 230000014616 translation Effects 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
- F16F15/06—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with metal springs
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B37/00—Pumps having pertinent characteristics not provided for in, or of interest apart from, groups F04B25/00 - F04B35/00
- F04B37/06—Pumps having pertinent characteristics not provided for in, or of interest apart from, groups F04B25/00 - F04B35/00 for evacuating by thermal means
- F04B37/08—Pumps having pertinent characteristics not provided for in, or of interest apart from, groups F04B25/00 - F04B35/00 for evacuating by thermal means by condensing or freezing, e.g. cryogenic pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/022—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using dampers and springs in combination
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/28—Counterweights, i.e. additional weights counterbalancing inertia forces induced by the reciprocating movement of masses in the system, e.g. of pistons attached to an engine crankshaft; Attaching or mounting same
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F7/00—Vibration-dampers; Shock-absorbers
- F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
- F16F7/104—Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted
- F16F7/116—Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted on metal springs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F7/00—Vibration-dampers; Shock-absorbers
- F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
- F16F7/1028—Vibration-dampers; Shock-absorbers using inertia effect the inertia-producing means being a constituent part of the system which is to be damped
Definitions
- the present disclosure provides cryocooler assemblies and methods and in particular embodiments, the present disclosure provides cryocooler assemblies and methods that can be utilized in conjunction with variable temperature analytical instruments such as cryostats.
- Cryocoolers (a.k.a. “coldhead”) have been used to vary the temperature of samples during analysis well into the low Kelvin range of temperatures. During this variation of temperatures, vibrations can exist which can substantially impact the analysis of the sample.
- the present disclosure provides a cryocooler that, in at least some embodiments, reduces vibrations.
- Cryocooler assemblies can include: a first mass configured to generate mechanical responses; a second mass operably engaged with the first mass; and an assembly between the first and second mass, the assembly configured to allow movement of the first mass in relation to the second mass.
- the methods can include: generating a mechanical response about a first mass within a cryocooler assembly; suspending the first mass in relation to a second mass of the assembly; and operatively engaging the second mass as a cold source for the cryocooler assembly.
- FIG. 1 is a block diagram of an analytical instrument according to an embodiment of the disclosure.
- FIG. 2 is a depiction of an assembly/instrument according to an embodiment of the disclosure.
- FIG. 3 is a depiction of an assembly/instrument according to another embodiment of the disclosure.
- FIG. 4 is a depiction of an assembly/instrument according to another embodiment of the disclosure.
- FIG. 5 is a cryocooler according to an embodiment of the disclosure.
- FIG. 6 is a cryocooler according to another embodiment of the disclosure.
- FIG. 7 is a cryocooler according to another embodiment of the disclosure.
- FIG. 8 is a cryocooler according to another embodiment of the disclosure.
- FIG. 9 is a cryocooler according to another embodiment of the disclosure.
- FIG. 10 is a cryocooler according to another embodiment of the disclosure.
- FIG. 11 is a cryocooler according to another embodiment of the disclosure.
- FIG. 12 is a cryocooler according to another embodiment of the disclosure.
- analytical instrument 10 includes a sample chamber 14 in operative communication with a cooling pod 12 that may include both a cooler 16 and a pumphouse 18 . While cooling pod 12 is shown housing both cooler 16 and pumphouse 18 , this is not necessary, but may be desirable as cooler 16 and pumphouse 18 may be housed separately but operatively coupled to one another and/or to sample chamber 14 . In accordance with an example implementation, there can be separation (thermal, vacuum/pressure, and/or physical) of sample chamber 14 from cooler 16 . Cooler 16 can include an operational coldhead for example. This is just one example of an instrument or assembly that can benefit from embodiments of this disclosure.
- instrument or assembly 210 a can include masses 212 and 214 respectively. These masses can be operatively engaged via another assembly 216 . In accordance with example implementations, both masses 212 and 214 may be in physical contact with a mounting surface 220 which may be the same or different surfaces. As a part of operating instrument or assembly 210 a , a device 218 is engaged that generates mechanical responses, such as vibrations. Device 218 can be a prime mover such as a pump, motor, gas mover, etc. and/or may provide either or both of high or low frequency noise. Mass 212 can be engaged with surface 220 via spring and damper assembly 222 .
- Spring and damper assemblies can include any assembly that includes: only a spring, only a damper, a spring and damper, but can functions to bias one mass in relation to another mass, one mass in relation to a surface, and/or both masses in relation to a surface.
- Spring and damper assemblies, pressure differences, and/or O-rings and/or assemblies can be utilized to suspend one mass in relation to another mass. The suspending of the masses can allow for motion between the masses in one, more, or all planes while still operatively engaging the masses. As one example, the coldhead motion in relation to the chamber of a cryocooler.
- Mass 214 can be engaged with surface 220 via spring and damper assembly 224 .
- the combination of the masses 212 and 214 with possibly different spring and damper assemblies 224 and 222 can provide a low pass filter connection to surface 220 .
- Providing different combinations of masses and springs and dampers can provide for a purposeful mismatch in resonance frequency between masses 212 and 214 as they are engaged by assembly 216 .
- Assembly 216 can include sliding complimentary components engaged by O-rings.
- assembly 210 b is depicted to demonstrate only one of masses 212 or 214 in physical contact with a mounting surface 220 with the other mass referenced to it.
- Mass 212 can be engaged with surface 220 via spring and damper assembly 222 and mass 214 can be engaged with mass 212 via spring and damper assembly 225 .
- assembly 210 c is shown that depicts a demonstration of yet another assembly configuration.
- Assembly 210 c has mass 214 engaged with surface 220 via spring and damper assembly 224 and mass 212 can be engaged with mass 214 via spring and damper assembly 223 .
- cryocooler assemblies 20 a - 20 e are depicted in FIGS. 5 - 9 .
- a cryocooler assembly 20 a is shown that includes a cold head 22 that is arranged as a first stage 24 and second stage 26 coldhead device.
- Coldhead 22 can be operatively coupled to a compressor system providing coolant fluid such as but not limited to nitrogen and/or helium, for example, or alterations thereof.
- coolant fluid such as but not limited to nitrogen and/or helium, for example, or alterations thereof.
- the coldhead can also be configured to provide a heat sink or cold source that can be linked to one or more masses to remove heat from or provide cooling to the one or more masses.
- System 20 a can include a chamber 27 that can be maintained at an interior pressure 30 that is substantially different than the exterior pressure 32 .
- This pressure differential can be utilized to provide suspension force on the coldhead 22 within chamber 27 as desired.
- coldhead support structures 34 can be placed about housing 28 of chamber 27 to provide for a sliding engagement of structures 34 and housing 28 , thereby suspending one mass in relation to another mass
- Sealing structure 36 can have improved functionality when compared to other implementations such as a rigid tube or bellows connection. For example, high resonance frequencies can be more effectively attenuated in all directions and modes (X-Y-Z translations, tip, tilt, and torsion between bodies 34 and 28 ) ultimately resulting in less mechanical energy transfer to body 28 and a lower resonance frequency of body 28 .
- assembly 20 b is depicted that includes spring and damper assemblies 38 - 41 that are arranged according to an embodiment of the disclosure.
- sealing structure 36 and assemblies 38 and 40 can maintain the pressure differential between the interior and exterior volumes, but also provide a damping of vibrations generated about the coldhead thus limiting the vibrations extending to a sample that is supported by a mass which is coupled to the coldhead.
- support structure 34 can include upper spring and lower spring and damper assemblies 38 and 40 , and coldhead 22 can be mechanically insulated from housing 28 .
- spring and damper assemblies 38 and 40 can be tuned specifically to attenuate vibration transfer from the coldhead and coldhead support to the rest of instrument, including surface 220 to which the spring and dampers 38 and 40 are mounted.
- the combined system of spring and damper assemblies 38 and 40 along with the coldhead mass can be purposefully de-tuned from the housing 28 mass and the spring and damper assemblies thus reducing the transmission of vibration from the coldhead to the housing 28 when mounted on common surface 220 .
- housing 28 can include upper spring and damper assembly 39 and lower spring and damper assembly 41 that can be tuned specifically, according to the mass and resonant frequency of the chamber, to reduce the vibrations of the chamber.
- assembly 20 c depicts another configuration that provides for the spring and damper assemblies 39 mounted between the housing 28 and support structure 34 that is operatively engaged with surface 220 via spring and damper assemblies 38 .
- assembly 20 d depicts another configuration having spring and damper assemblies 39 operatively engaged between support structure 34 and housing 28 . Housing 28 may also have spring and damper assemblies 41 operatively engaged with surface 220 .
- assembly 20 e depicts another configuration without a spring and damper assembly engagement to support structure 34 . Assembly 20 e can rely on the pressure differential between interior pressure 30 and exterior pressure 32 to support the mass of coldhead 22 and support structure 34 . Accordingly, only housing 28 may be operably engaged with the surface 220 via spring and damper assemblies 41 in this specific embodiment.
- coldhead 22 and supports 34 of FIGS. 5 - 9 can correspond to mass 212 of FIGS. 2 - 4
- housing 28 of FIGS. 5 - 9 can correspond to mass 214 of FIGS. 2 - 4
- the arrangement of spring and damper assemblies can likewise correspond according to example implementations.
- cryocooler assemblies 400 a - b are shown providing at least some of the contemplated cryocooler configurations.
- Each cryocooler can include a coldhead 22 having operable stages 24 and 26 , for example.
- About the coldhead and stages can be a housing 28 that defines a chamber 27 .
- a temperature gradient 25 can exist within chamber 27 .
- a liquid form of the cryofluid can exist and this may have the lowest most temperature of the cryofluid within the chamber.
- the cryofluid may exist as a gas/liquid or as a gas and these temperatures are different, (higher) than the temperature of the liquid at the lower most portion of the chamber.
- thermally conductive masses such as masses 42 , 44 , 60 , and/or 62 can be thermally engaged with the cryofluid within the chamber.
- This thermal engagement can be convective, conductive, and/or a combination of both.
- masses 42 , 44 , 60 , and/or 62 can be thermally engaged via convections 45 , 47 , 65 , and/or 67 respectively. Accordingly, these masses have the temperature of the cryofluid with which they are thermally engaged.
- these masses may be conductively engaged with both the cryofluid and the coldhead via respective thermal links 46 , 48 , 64 , and/or 66 .
- These thermally conductive links and/or masses may be constructed of thermally conductive materials such as copper.
- the masses can be arranged in relation to the cryofluid to maintain the masses at a desirable temperature for use as a cold source for discrete portions of a cryoanalytical device.
- cryocooler assemblies can include at least one thermal link extending from a coldhead 22 within chamber 27 .
- assembly 400 a is shown that includes separate thermal links 46 and 48 extending from corresponding first and second stages 24 and 26 of coldhead 22 within chamber 27 . While two links are depicted in this configuration, a single link from the coldhead is contemplated.
- specific portions of the coldhead can be in thermal connection with specific masses 42 and 44 via respective thermal links 46 and 48 .
- the spring and damper assemblies can be tuned to minimize vibrations transfer from the coldhead to mass 42 and mass 44 .
- this thermal communication can include, but is not limited to: flexible conductive lines; and/or conduction and/or convection through the cryofluid within chamber 27 .
- the thermal links can allow for large relative motion between the masses 42 and 44 and the respective thermal connection points thus leading to an additional mechanical isolation.
- Masses 42 and 44 can also be suspended from coldhead stages 24 and 26 through a spring and damper assembly that is not depicted here, or mounted to housing 28 through a spring and damper assembly that is not depicted, but also contemplated.
- assembly 400 b is depicted that includes portions 42 and 44 of chamber housing 28 . These portions can be thermally conductive while other portions of chamber housing 28 are insulative.
- thermal gradient 25 may exist in the cryofluid contained within the chamber 27 and the thermal masses 42 and 44 may be positioned at different heights, for example near the second stage 26 and/or first stage 24 of the coldhead for example, to utilize different temperatures along the temperature gradient of the fluid, and the associated cooling powers.
- thermal links 45 and 47 can provide cold source links as a liquid or gas thermal link between the contents of the chamber the proximate mass.
- masses 52 and 54 are in thermal communication with thermally conductive portions 60 and 62 respectively via thermal links 56 and 58 These contacts are in thermal connection, via flexible conductive lines and/or conduction and/or convection through the cryofluid, with the coldhead via additional links 64 and 66 and/or convections 65 and 67 .
- spring and damper assemblies 39 and 41 can be tuned to minimize vibrations transfer from the coldhead to mass 52 and mass 54 .
- masses 52 and/or 54 can define portions of a cryoanalytical device utilizing and/or associated with the cryocooler assembly.
- the portions of the cryo analytical device can include a radiation shield or a sample mounting surface or fixture.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Sampling And Sample Adjustment (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Abstract
Description
Claims (7)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16/597,655 US12071998B2 (en) | 2018-10-09 | 2019-10-09 | Cryocooler assemblies and methods |
| US18/815,483 US20240416352A1 (en) | 2018-10-09 | 2024-08-26 | Cryocooler Assemblies and Methods |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201862743482P | 2018-10-09 | 2018-10-09 | |
| US16/597,655 US12071998B2 (en) | 2018-10-09 | 2019-10-09 | Cryocooler assemblies and methods |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US18/815,483 Continuation-In-Part US20240416352A1 (en) | 2018-10-09 | 2024-08-26 | Cryocooler Assemblies and Methods |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20200109763A1 US20200109763A1 (en) | 2020-04-09 |
| US12071998B2 true US12071998B2 (en) | 2024-08-27 |
Family
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Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US16/597,655 Active 2039-11-09 US12071998B2 (en) | 2018-10-09 | 2019-10-09 | Cryocooler assemblies and methods |
| US16/597,680 Abandoned US20200109764A1 (en) | 2018-10-09 | 2019-10-09 | Cryocooler Assemblies and Methods |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US16/597,680 Abandoned US20200109764A1 (en) | 2018-10-09 | 2019-10-09 | Cryocooler Assemblies and Methods |
Country Status (3)
| Country | Link |
|---|---|
| US (2) | US12071998B2 (en) |
| DE (1) | DE112019005051T5 (en) |
| WO (1) | WO2020076988A1 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10775285B1 (en) | 2016-03-11 | 2020-09-15 | Montana Intruments Corporation | Instrumental analysis systems and methods |
| US12253205B1 (en) | 2018-09-28 | 2025-03-18 | Montana Instruments Corporation | Thermal transfer line assemblies, methods of manufacturing thermal transfer line assemblies, and thermal transfer methods |
| US11956924B1 (en) | 2020-08-10 | 2024-04-09 | Montana Instruments Corporation | Quantum processing circuitry cooling systems and methods |
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Also Published As
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| US20200109763A1 (en) | 2020-04-09 |
| WO2020076988A1 (en) | 2020-04-16 |
| DE112019005051T5 (en) | 2021-07-01 |
| US20200109764A1 (en) | 2020-04-09 |
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